How to Calculate Pressure Exerted by an Engine in a Vacuum?

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Discussion Overview

The discussion revolves around calculating the pressure exerted by an engine in a vacuum, specifically in the context of a lander landing on Mars. Participants explore different approaches to determining this pressure, considering both static and dynamic pressure components.

Discussion Character

  • Exploratory, Technical explanation, Debate/contested

Main Points Raised

  • One participant inquires about using the formula P=F/A to calculate pressure exerted by exhaust on a surface in a vacuum.
  • Another participant suggests that for pressure from a moving fluid, static pressure is equal to velocity pressure, and that P=F/A applies.
  • A follow-up question asks for clarification on the role of dynamic pressure in the calculations.
  • A later reply presents a formula for total pressure that includes static pressure, hydrodynamic pressure, and a term for dynamic pressure based on bulk velocity.

Areas of Agreement / Disagreement

Participants present different views on the relevance and calculation of dynamic pressure, indicating that there is no consensus on how to approach the problem.

Contextual Notes

The discussion does not resolve the relationship between static and dynamic pressure in this context, nor does it clarify the assumptions behind the proposed formulas.

Space259
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Hello all,

How would I calculate the pressure exerted on a surface by an engine in a vacuum, for example, if a lander was landing on Mars, I'm trying to calculate the pressure exerted on the surface by the exhaust. Should I simply be looking at P=F/A or should I be looking at dynamic pressure?

Thanks in advance
 
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For pressure exerted on a surface by a moving fluid perpendicular to it, the static pressure is equal to the velocity pressure, and p=f/a applies.
 
Last edited:
Hi Russ,

Thanks for your reply, so where does the dynamic pressure come into it? If you were to calculate the Dynamic Pressure what would you be calculating?
 
total pressure = P_hyd + P_stat + 1/2 * Rho * V^2
(V is bulk velocity)
 

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